Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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- 1. A pump station design fills a pressurized water tank by pumping water from a reservoir. The flow rate is 0.75 cfs. The pump is 10 feet above the reservoir, and the water tank is 100 ft above the pump. The pressure in the water tank is 10 psi. The suction and discharge lines are both (actual diameter) 6-inch Sch 40 steel (pipe roughness = 0.00015 ft). Use a kinematic viscosity of 1.21 x 10-5 ft²/s. Total pipe length is 200 ft. The suction line is 10 ft. You must account for friction loss, but you can neglect the minor losses. a. What is the head added by the pump in ft? b. What is the power added by the pump in HP (recall 1 HP = 550 ft*lb/s)? 110 ft 10 ft 0 ftarrow_forwardFluid 1arrow_forward4. Evaluate the pressure at the center of pipe A. Given: y of Liquid 1 = 12 kN/m y of Liquid 2 = 25 kN/m. hi = 60 cm h2 = 10 cm L = 60 cm а. -750 Рa c.-650 Pa b. -800 Pa d. -700 Pa Liquid 1 Liquid 2 h, h2arrow_forward
- Water in the reservoir is used to control the water pressure in the pipe at A. Take pHg = 13550 kg/m³ and p = 1000 kg/m³ Neglect the diameter of the pipe. (Eigure 1) Figure AQ B E h 400 mm C 150 mm 100 mm 200 mm Mercury pe he Y Part A If h= 140 mm, determine the gage pressure in the pipe at A when the mercury is at the elevation shown. Express your answer to three significant figures and include the appropriate units. PA 76.8 Submit 4 Provide Feedback kPa CINC Previous Answers Request Answer ? X Incorrect; Try Again; 4 attempts remainingarrow_forwardH.W.11// Determine the gage pressure at the center of pipe A in pounds per square to kN inch and in kilopascals. Ym = 133 m3 Water Air 328A 40 cm 131t Mercuryarrow_forwardQ2- The inverted U-tube manometer of Figure contains oil (SG 0.9) and water as shown. The pressure differential between pipes A and B, pA pB, is 5 kPa. Determine the differential reading h. 0.2 m 0.3 m Waterarrow_forward
- Q4) Water flows through a contraction section as shown. A pressure gage connected between the upstream pipe and throat section sk difference of Ap = 5 kPa. The gasoline velocity in the throat section is V2 = 3 m/s. What is the velocity V1(m/s) in the upstream pipe? V shows a pressure V2 AParrow_forwardAnswer fastarrow_forwardWater flows steadily downward through the pipe shown in the figure below. Viscous effects are negligible, and the pressure gage indicates the pressure is zero at point (1). Determine (a) the flowrate and (b) the pressure at point (2). (a) Q = (b) p2 = 2.1ft 3.1ft ↓s -0.12 ft (1) 5 -0.1 ft -free jet ft³/s lb/ft²arrow_forward
- Calculate the pressure at point A in the manoter shown. beight b'c = 0.50marrow_forwardA piston/cylinder receives R1343 at 300 Pa and compresses it in a reversible adiabatic process to 1000 kPa. 60-C. Find the tempature and sketch the p-v and T-s diagramsarrow_forwardWater flows in a steel pipe (e = 0.00020 feet) at a flow Q = 12.5 cfs. The diameter of the pipe is D = 18 inches and the length of the pipe is L = 2,500 feet between section 1 and section 2. The elevation at section 1 is z = 100 feet above the datum. The elevation at section 2 is z2 = 75 feet above the datum. The temperature of the water is 70°F. The kinematic viscosity of the water is 1.06 x 10° ft/s. The pressure at section 1 is p1 = 90 psig (pounds per square inch gage). a) Determine the velocity v in feet per second (fps). b) Determine the Reynolds number Re. c) Classify the flow based on the Reynolds number Re. d) Determine the Darcy-Weisbach friction factor f. e) Determine the friction head loss hfäic in feet in the pipe between section 1 and section 2. f) Determine the pressure p2 in psiq at section 2.arrow_forward
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